3A-12 P/N 13999-002 Info Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
Electric Trim/Autopilot Failure
Any failure or malfunction of the electric trim or autopilot can be over-
ridden by use of the control yoke. If runaway trim is the problem, de-
energize the circuit by pulling the circuit breaker (PITCH TRIM, ROLL
TRIM, or AUTOPILOT) and land as soon as conditions permit.
1. Airplane Control ......................................... MAINTAIN MANUALLY
2. Autopilot (if engaged) .....................................................Disengage
If Problem Is Not Corrected:
3. Circuit Breakers................................................ PULL AS Required
• PITCH TRIM
• ROLL TRIM
•AUTOPILOT
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke................................. MANUALLY HOLD PRESSURE
6. Land as soon as practical.
September 2011
To Next Page
Loading...
